Temperature measurement of molten metal



. MACHLER ETAL TEMPERATURE MEASUREMENT OF MOLTEN METAL Filed July 11, 1949 4 sheets-she t l mam-m Q MAGHLER wnumum G. msn'm T mam J y 1954 R. c. MACHLER ET AL 3, 88

TEMPERATURE MEASUREMENT OF MOLTEN METAL Filed July 11, 1949 4 Sheets-Sheet 2 WWEMTORS RAYMOND G. MAGHLEW WHILMAM FMSTBE MTTQRNEYS y 20, 1954 R. c. MACHLER ETAL ,683,988

TEMPERATURE MEASUREMENT OF MOLTEN METAL Filed July 11, 1949 4 Sheets-Sheet 3 Fig. 4

1 I I Z Z Z/ em 83 7 F 9. w f /I ///Z r /f INVENTORS RAYMOND C. MAGHLER BY WlLLlAM G. FASTIE Wh &

ATTORNEYS y 1954 R. c. MACHLER ETAL 88 TEMPERATURE MEASUREMENT OF MOLTEIN METAL Filed July 11, 1949 4 Sheets-Sheet 4 Fig.7

INVENTORS RAYMOND G. MAGHLER WILLIAM G. FASTflE ATTORNEYS Patented July 20, 1954 TEMPERATURE MEASUREMENT OF MOLTEN METAL Raymond C. Machler, Philadelphia, and William G. Fastie, Willow Grove, Pa., assignors to Leeds and Northrup Company, Philadelphia, Pa., a corporation of Pennsylvania Application July 11, 1949, Serial No. 103,996

9 Claims.

This invention relates to methods and apparatus for determining the temperature of molten metal or other liquid by measurement of radiation therefrom.

In determining the temperature of a liquid such as a stream of molten metal during the tapping of a furnace, errors occur in the measurements made with a radiation pyrometer due to the formation of an oxide film or slag on the surface of the metal, irregularities in the surface or sunlight falling on the surface. The variability of the radiation, due to variations in the emissivity of the surface, as the molten metal flows from the furnace makes it difiicult to obtain the true metal temperature.

In the use of a radiation pyrometer for measuring the temperature of a material, in order to determine its true or actual'temperature, it is necessary either that the emissivity value of the material be known so that the proper correction factor can be applied to the pyrometer reading, that the material be, in fact, a black body so that no correction need be applied, or that the temperature measurements be made under black-body conditions. Heretofore, measurements of the temperature of the surface of a stream of molten metal have not been taken under black-body conditions.

In accordance with the invention, the true temperature of a moving body of molten metal or other heat-radiating liquid is determined by effecting rotation of the liquid to produce a vortical cavity whose sides and closed bottom are defined by the liquid thus to establish black-body conditions for which the radiation observed by sighting into the cavity is unaffected by variations in emissivity of the particular liquid or by the different emissivities of different components of the liquid.

More specifically, in some forms of the invention a stream of molten metal is directed tangentially of a vessel having a discharge passage extending centrally of its bottom so to form a vortical cavity in the molten metal; in other forms of the invention, a sample of molten metal is raised in a. dip bucket having tangential channels or equivalent internal passages causing the metal to form a vortex as it flows out of a restricted discharge opening in the bottom of the bucket.

For a more detailed disclosure of the invention and for further objects and advantages thereof, reference is to be had to the following description taken in conjunction with the accompanying drawings, in which:

Fig. 1 diagrammatically illustrates a radiation pyrometer installation including a transverse vertical section taken on the line I-l of Fig, 2 of a device for forming a vortex in a liquid stream;

Fig. 2 is a top view of the vortex-forming device shown in Fig. 1;

Fig. 3 is an elevational view, partly in section, of an installation for measuring the temperature of a stream of molten metal as it issues from the trough of a furnace;

Fig. 4 is a plan view of a modification of the vortex-forming device shown in Fig. 2;

Fig. 5 is a transverse vertical section taken on line 5--5 of Fig. 4 with a cutaway view of the liquid cavity formed by the vortex-forming device;

Fig. 6 is a diagrammatic view, partly in section, of a vortex-forming device, or dip bucket, as employed for determining the temperature of a liquid while in a ladle or similar container; and

Fig. 7 is a top view of the dip bucket shown in Fig. 6.

The true temperature of a material may be directly determined with a radiation pyrometer only when the measurements are taken under black-body conditions: otherwise, it is necessary to correct the readings by reference to charts or tables correlating the observed and true temperatures of materials having different emissivities.

However, in many instances, it is not possible to take pyrometer measurements under blackbody conditions: for example, in certain types of furnaces, such as cupolas and blast furnaces, the particular construction of the furnace does not permit a, radiation pyrometer to be sighted into the molten charge. In this type of situation it becomes necessary to measure the temperature of the molten metal after it is discharged from the furnace and where black-body conditions do not normally exist. Such temperature measurements may be taken as the molten metal issues directly from the furnace or possibly after the liquid has been discharged into a ladle so that its temperature may be checked before pouring.

Referring to Fig. 1, as exemplary of apparatus suited for achieving the purpose of the invention, there is shown a discharge trough iii of a furnace II from which a liquid stream such as a stream of molten iron [2 is flowing. As the liquid l2 flows from trough Ill it enters channel I3 of the vortex-forming device or body member M which provides a connecting passageway with a body cavity 15, also located in member is. The channel i3 joins the body cavity 5 at an angle tangent to the opening in the tubular flow passage or discharge orifice 16 of body cavity it. Thus, the liquid stream is caused to flow tangentially into the body cavity l5 thereby attaining a rotary motion and causing a vortex l? to be formed therein. A cavity l'i'c having a closed end or bottom Ho and an open end or top is formed by the molten metal along the axis Ila of the vortex 11, and its resultant shape is controlled by the physical dimensions of the tubular flow passage N5 of the vortex-forming device i i. A more detailed description of the formation of the device it will be hereinafter given. The liquid stream 52 continues its fiow from the tubular discharge orifice l6 and is received in a iorehearth E3 or other suitable container.

The vertical cavity 170 of molten metal is a black-body cavit It provides a source of radiation formed by the bottom closure and the wall oi liquid rotating at a speed adequate to maintain it in spaced relation from the central portion of the cavity.

A black body as herein contemplated is one having theoretically maximum emissivity, and to that maximum emissivity is customarily assigned the numerical coefiicient or emissivity value of unity. All other materials, including those normally met with in practice and whose temperatures are to be determined, have emissivity values less than the aforesaid arbitrary black-body constant of unity, and are known as non-black bodies, which term includes gray bodies, whose emissivity coefficients are substantially constant throughout the range of wavelengths of utilized radiation, and bodies having selective radiation whose emissivity coefficient is not the same at different wavelengths.

As shown in Fig. 1, a radiation pyrometer unit or head [9 may be sighted along the axis Ha of the vortex i1, and since the cavity I70 formed by the liquid stream i2 establishes black-body conditions, the true temperature of the metal is directly determined, obviating need for emissivity tables or charts. Such radiation pyrometer unit is preferably of the multicouple type disclosed in Letters Patent 2,232,594 granted to P. H. Dike, for producing an electromotive force representative of the quantity of radiation entering the lower or sighting end or" the unit i9. The black-body radiation from the bottom and walls of the cavity He is directed upon the target of a thermocouple device or thermopile within the unit L9, as disclosed in the Dike patent, to produce an electromotive force whose magnitude, representative of the true temperature conditions of the liquid, is measured in any suitable manner, preferably by the potentiometric method.

The potentiometer network 20 comprises a slidewire resistance 21 traversed by current of standardized magnitude supplied from a suitable source of current, such as battery 22. To avoid crowding of the scale 23 associated with the movable contact 24 of the slidewire, there is provided the usual end coil 25. The standard cell usually used during adjustment of the slidewire current to standard magnitude is not shown; it suflices here to say that the rheostat 26 is adjusted to produce a predetermined difference of potential between the points 2? and 28 of the potentiometer network, which potential is substantially equal to or at least not less than the potential developed by the thermopile for the maximum radiation it is to receive from the effectively closed end or Walls of the body cavity.

bottom and the walls of the cavity l'lc of the vortex i! as viewed from above. For determination of the temperature of the liquid stream, the contact 24 is adjusted until there is no deflection of the galvanometer 29, the null deflection indicating balance of the voltage developed by the thermopile against the voltage drop between terminal 21 and contact 24 of the potentiometer network due to flow of the slidewire current. The balancing of the potentiometer may be effected manually, or by a self-balancing mechanism generally of the type shown in Leeds Patent 1,125,699 or Squibb Patent 1,935,732, which is provided with a scale and. a'chart, generically represented by scale 23, for indicating and/or recording the temperatures.

In Fig. 2 there is shown a top view of a body member or vortex-forming device M as shown in section in Fig. 1. By a means such as the vortex-forming device 14, a black-body cavity may be formed as a target in the liquid stream and the true or actual temperature of the liquid determined by sighting on the target a radiation pyrometer which is capable of converting the black-body radiation emanating from the vortical cavity into an indication related to the temperature of the liquid stream. The device M is constructed from a heat-resisting or refractory material and has a flow passage having cavity portions l3 and 55 respectively defining a downwardly sloping channel I3 which tangentially joins a funnel-shaped cavity 15. The funnelshaped cavity 15 has a tubular flow passage or discharge orifice it and intermediate the far end of the channel 13 and the cavity I5 is located an overflow opening 36 for discharging slag and any excess liquid due to an abnormally large flow from the furnace. Overflow orifice 39 may also serve as a safety or by-pass opening if for any reason the tubular flow passage [6 of the cavity i5 should become stopped up or clogged so that it would no longer be able to discharge the normal furnace flow for which it was designed. As shown in Fig. 1 the channel 3| which connects overflow orifice 39 with channel 13 has a crest 32 which joins the wall of channel 13 at a point slightly below the height attained by the normal flow of liquid from the furnace through the channel [3. The crest 32 of overflow channel 3i is of such height that the amount of metal flowing into body cavity I5 is never great enough to close the passage is and so effectively destroy the desired deep cavity to be formed in the liquid. A slag skimmer 33 bridges the channel l3 and is positioned between the overflow channel 3i and body cavity 15.

For a good cavity formation in the liquid over a wide range of fiow the shape and size of the flow-passage in block [4 for a particular closure is of importance. As indicated in Fig. 1, a desirable shape is a long closed-bottom liquid cavity,

such as cavity [10, which will not be influenced by the height of liquid in the forehearth i8 so long as the level does not reach the point of closure: the closed bottom ill) of the cavity He may, as in Fig. 1, be formed considerably below the discharge end of flow passage It. In order to ob tain symmetrical flow into the tubularfiow passage 16, it is necessary to have a considerable amount of rotary motion of the liquid above the tube. This rotary motion is obtained by directing the liquid stream into the body cavity I5 tangentially to the flow passage It, so to produce a uniformly highhead of liquid allaroundthe Since the angular momentum of the liquid persists in the tubular section, if the discharge tube is very short in length, the high angular momentum or rotary motion at the bottom of the tube will cause an umbrella-shaped discharge of the liquid. It is possible for such a discharge to be terminated by the liquid in the forehearth (Fig. l) to form a black-body cavity for pyrometric purposes; however, such procedure is subject to the objection that if a particle of foreign matter becomes lodged in the mouth of the discharge opening a break will appear in the surface of the urnbrella-shaped closure and black-body conditions will no longer be obtained. By selecting longer lengths of tubes the tendency of the discharging liquid to fiare out into an umbrella-shape is decreased due to the resultant reduction of the angular momentum or rotary motion of the liquid within the tube caused by the additional friction resulting from the additional length of tube. While a considerable amount of angular momentum is desirable at the outer edges of the vortexforming device in order to obtain a good distribution of the liquid, nevertheless, excessive angular momentum in the orifice tube is undesirable since it would require an impractical length of tube to reduce the angular momentum of the fluid sufficiently to permit a closure.

In a specific application, an orifice [6, Figs. 1 and 2, having a 1 inch opening and approximately 3 inches to 3 inches in length produced consistently good cavity formation over a flow range of from cubic foot per minute to cubic foot per minute. The cavities roduced had a diameter of approximately of an inch and ranged in length from five inches for a height of liquid at the maximum diameter of cavity l 5 of at inch to eleven inches for a corresponding height of 1 inch. In another application, it was found that a vortex-forming device l4 having a discharge orifice I6 with an opening of approximately 1 inch in diameter would handle satisfactorily a flow of molten iron from a cupola at an approximate rate of 600 pounds per minute. By increasing the diameter of the opening to approximately 1 inches, the rate of flow was readily increased to approximately 750 pounds per minute.

In Fig. 1 the trough it represents existing foundry equipment. In practice it may have a width of six inches while the Width of the molten metal stream may be of the order of two inches. Under these conditions the channel i3 in the vortex-forming device [4 may be of the order of two and one-half to three inches wide with a corresponding width of cavity I 5 of from 6 inches to 7 inches. The length of channel It may vary and is not particularly critical; however, it is preferable that it be designed so that when the vortex-forming device is mounted adjacent to the end of the furnace trough very little change, if any, in the normal discharge stream position will be caused. The overflow opening 30 should be sufficiently large to take care of the maximum rate of fiow from the furnace, and it should be located in such a position that the metal discharged therefrom will fall in a smooth stream in reasonable proximity to the stream issuing from the vortex within tube [6.

The vortex-forming device l4 should be constructed from a suitable refractory material such as fire-clay or clay-graphite and should be of sufficient thickness to afford adequate mechanical strength and thermal insulation. The tubular orifice It may be an integral part of the block I4 formed either within it as shown in Fig. l or as a protruding extension. It may also be formed separately if so desired and then assem bled into a mating opening in the block.

In a specific application a vortex-forming device M was molded from a mixture consisting of three parts Berlite and one part No-Joint, as made by the Ironton Fire Brick Company, Ironton, Ohio. The materials were thoroughly mixed while dry, then moistened slightly, and rammed into a mold. The mold was removed and the vortex-forming device [4 was dried in a core oven at a temperature of approximately 400 F. to 450 F. for a period of approximately 5 hours to 6 hours. A vortex-forming device constructed in such a manner was found to give satisfactory results and would last under continuous operation for a period of 5 or 6 days with only minor patching being needed.

In Fig. 3 is shown an installation of the invention for measuring the temperature of a stream of molten metal as it leaves the trough of a furnace. Upon leaving the trough 40 of a furnace 39, the metal stream 38 flows into the vortexforming device M which is constructed from a refractory material and is supported by a platform 42 from standard 43. The metal stream enters the vortex-forming device or body member M at the adjacent end of channel 44 and flows therethrough until it reaches the opposite end of the channel whereupon it is directed tangentially into body cavity 55. Due to the rotary motion imparted to the metal stream, a vortex forms therein having an elongated cavity 66 effectively closed at its bottom extending through the tubular flow-passage 47, the latter serving as a discharge orifice for the body cavity 45. The liquid is ultimately received into a tilting forehearth 4 8 or some other form of container cus tomarily employed in foundry practice. The vortex forming device 4! is provided also with a relief channel 58 and an auxiliary discharge opening 59 for by-passing any excessive amount of fiow from the furnace. A slag skimmer 6| bridges the channel 44 and. is similar to the slag skimmer 33 shown in Figs. 1 and 2.

Directly above the body cavity 45 and supported from an arm 43 on the standard 33 is located a radiation pyrometer unit 53 preferably of the type disclosed in the Dike Patent 2,232,594, and as previously briefly described in connection with Fig. 1. The indicator and recorder with their associated circuit have been shown symbolically by instrument 6G in Fig. 3. The pyrometer unit as shown in Fig. 3 is equipped with a cooling jacket '5! and an open-end sighting tube 52. The sighting tube '52 of unit 59 is so positioned that it is coaxial with the axis of the elongated closed cavity 46 formed by the molten metal stream. By means of the supporting structure 43, 42 and 49 and associated fastening means, the pyrometer unit 50 and the vortex-forming device 4| can be held in proper alignment, thus constancy of alignment between the pyrometer 5G and the target formed by the cavity =26 in the molten metal stream will be assured.

In order to prolong the life of the pyrometer and to insure accurate measurements, an air supply, indicated by line 53, valve 5H and filter 55, is provided for cooling the unit 59 and purging the sighting tube 5-2 of fumes, dust, etc. The air line 53 is connected to cooling jacket Si in such a manner that the air is directed along the unit 50 and in actual contact with it. Since the volume of air required for cooling the pyrometer may be greater than the volume of air required to purge the sighting tube, provision is made as by openings 56 to divert some of the air so that only the proper amount will enter the tube. To protect the pyrometer from direct radiation from the molten metal a suitable radiation shield 51 is provided. As a further aid in keeping the assembly cool,- the air that is diverted from the cooling chamber through openings 56 may be directed against the shield 57. Other adjustable mounting arrangements and cooling jackets adaptable to this application are disclosed in the Dike Patent 2,232,594 and Mead Patent 2,275,265.

In Figs. 4 and 5 is shown a further modification of the vortex-forming device M, previously described and illustrated in Figs. 1 and 2. In Figs. 4 and 5 the body member or vortex-forming device 80 is provided with a flow passage comprising an inlet channel 8! and a discharge tube 82, the latter having a sloping lip 83 which is similar to the sloping wall of a funnel. The inlet channel 8| joins the sloping portion 33 at a point tangent to the circumference thereof and extends completely' therearound forming a fiat ledge 8ia of decreasing width, the outer edge thereof having the curvature of a spiral. By providing an extension of channel M in the form of the ledge 8M, extending completely around the sloping portion 83, substantial coaxial alignment of the liquid cavity 84 and the discharge tube 82 may be maintained over a wide range of flows thus insuring coaxial alignment of the liquid cavity and the pyrometer unit time the two have been aligned. The sloping portion 83 has been shown with an incline of approximately 5 with respect to the horizontal plane of ledge am and may vary throughout the approximate range of 0 to 20. If a slope much greater than 20 is provided, the liquid l2 from the furnace Ii will be discharged through the tube 82 into the container IS with such high angular momentum that there will be no formation of an elongated cavity 84 in the liquid. While the slope of the inclined portion of body cavity IS in Figs. 1 and 2 has been shown as approximately 20 it is to be understood that it may also vary within the aforementioned range.

In a specific application of the modification shown in Figs. 4- and 5, the vortex-forming device 80 was constructed from a heat-resisting material commonly known as clay-graphite and was provisited with a discharge opening 2 inches in diameter and approximately 3 inches in length. The outer diameter of the sloping portion 83 was approximately 5 inches and the length of the channel 85 from the liquid receiving end to its point of tangency with the circumference of slop ing. portion 83 was approximately 7 inches to 8 inches. The depth of the channel 8! was approximately 6 inches which in combination with the relatively large diameter or discharge opening 82 provided suflioient capacity to handle a relatively wide range of flow without the need of an over-flow such as opening is shown in Figs. 1 and 2. While neither an overflow opening nor a slag skimmer has been shown for the vortexforming device 80 in Figs. e and 5, it is to be understood that either or both may be provided in a manner as previously described in connection with the vortex-forming device It shown in Figs. 1 and 2. It is also to be understood that the vortex-forming device 80 may be used in either of the pyrometer installations shown in Figs, 1 and 3 in place of the vortex-forming devices l4 and H shown therein.

For the purpose of clarity the liquid l2 has not been shown in Fig. 4. In Fig. 5 the liquid has been shown only as it enters the vortex-forming device 8i) and as it is being discharged from the tube 82 after formation of the cavity 84 in order that the interior of the vortex-forming device 80 may clearly be seen.

As shown by Figs. 6 and 7, the invention may also be applied to measure the temperature of samples of molten metal or other liquid 64 in a ladle prior to its being poured into molds or the like. The vortex-forming device or dip bucket 65 is shown (Fig. 6) in a suspended position be-' tween iadie 3S and the radiation pyrometer unit [9. From this position the dip bucket 65 is first lowered by any suitable arrangement, as indi cated by the solid arrow, into ladle 66 where it is filled with a sample of the molten metal 64. The clip bucket is then raised, as indicated by the broken line arrow, above the surface of the liquid Gd to a predetermined position with respect to the radiation pyrometer iii. A rotary motion is im-' parted to the molten metal (34 in the dip bucket by providing tangentially extending passages 61 in the wall of the bucket and allowing the metal to enter the bucket through such passages, thus producing a vortical cavity 68 and providing black-body radiation from the molten metal. The cavity wall rotates at a speed adequate to maintain it in spaced relation from the central portion of the cavity 68, and due to the shape of the tubular discharge flow passage 69 the vortical cavity of molten metal is caused to close at its bottom and thereby form a black-body target into which the radiation pyrometer i9 is sighted. The radiation pyrometer I9 is mounted in such a position that it may be sighted directly into the cavity as and suitable means may be provided so that there will be a constancy of alignment between the dip bucket and the pyrometer when the former is in a predetermined raised position preparatory to a measurement being taken. In this connection, it should be pointed out that the dip bucket 65 and the radiation pyrometer I9 may be connected together in a fixed spaced relation so that the dip bucket and pyrometer may be raised and lowered as a unit, thim assuring constancy of alignment of the two at all times.

The leads 10 of the radiation pyrometer unit l9 may be connected to a measuring circuit such as previously shown and described in connection with Fig. 1.

In Fig. '7, which is a top view of the vortexforming device or dip bucket 65, the tangential passages 81 are shown by the broken lines and are relatively large in diameter as compared to the diameter of flow passage 69. While the tangential passages 6! have been shown as tubular in shape and having a circular cross section, it is to be understood that they may be formed with other cross sectional shapes such as rectangular, elliptical, etc., and may take the form of open channels similar to channel l3 shown in Figs. 1 and 2. The proportions of the tubular flow passage 69 may be similar to those previously described in connection with the flow passage l6 as shown in Figs. 1 and 2.

Thus, in the intermittent measuring method of Figs. 6 and 7, as Well as in the continuous method of the previous modifications, the molten metal or the like is caused to flow in a vortex into which a pyrometer is sighted for direct measurement of true temperature under black-body conditions.

While this invention has been described in connection with a total-radiation pyrometer shown in Fig. 3 as unit 50 and in Figs. 1 and 6 as unit I9, it is to be noted that it may be replaced by any equivalent automatic viewer and may be replaced by an optical, or partial-radiation pyrometer and a human operator who sights through tube 52 upon the elongated cavity in the molten metal vortex to determine the temperature of the metal.

The increase in accuracy of temperature meas urements obtained by use of a pyrometer in combination with a vortex-forming device as com pared with the measurements obtained in sighting a radiation or optical pyrometer upon a fiat or usual surface of liquid will now be pointed out. sighting upon the usual surface of a liquid having a true temperature of 1400 C. and a surface emissivity of 0.4 the temperature indication of an optical pyrometer will be 1275 C. or in error by 125 C. from black-body conditions (emissivity 1.0). A change of surface emissivity to 0.5 will result in a change of temperature indication of the optical pyrometer to 1307 C. or a total change of 32 C. for a change of emissivity from As aforementioned the purpose of the present invention is to increase the effective emissivity of the surface of the liquid so that the temperature measurements thereof may be made under substantially black-body conditions and thereby reduce the amount of error introduced due to variations in the emissivity of the surface. The increase in accuracy of temperature measurements obtained by the use of an optical pyrometer with the vortex-forming device may best be described by reference to an article concerning the change in effective emissivity when the surface of a liquid is formed into a cavity. The article to which reference is made is, Emission Factor of Cavities of Simple Geometric Shape," Comptes Rendus Acad. Sci, Paris, vol. 2 6, pages 999-1000, March 22, 1948. The geometric shape which corresponds approximately to the shape of the liquid cavity formed by use of the vortexforming device is that of a cylinder. In the above article bymeans of a mathematical formula disclosed therein a table of values was compiled and a chart drawn showing the relationship of the effective emissivity of the interior of a cavity to the emissivity of a flat surface of the same material for different ratios of L/R; where L is the depth of the cavity and R is the radius of its opening. Thus, as the L/R ratio increases for a cavity of any simple geometric shape such as a cylinder, sphere or. cone, the effective emissivit of the cavity also increases and may be readily calculated.

In the specific application of the invention aforementioned in connection with Figs. 1 and 2, the smallest L/R ratio referred to was approximately 13 to 1: L being 5 inches and R being inch. By reference to the formulas mentioned in the aforementioned article a surfac having an emissivity of 0.4 when it is in its flat or usual condition will have an effective surface emissivity of 0.966 when formed into a cavity having an L/R ratio of 13 to 1. By increasing th eifective emissivity of the surface in this manner an ideal optical pyrometer will now indicate a surface temperature of 1396 C. If the surface emissivity should change to 0.5 then the cavity emissivity would change to 0.978 and the ideal optical pyrometer would indicate a temperature of 1397 C. Comparing the effects of the change Employing the conventional method of of surface emissivity shows that a change of surface emissivity from 0.4 to 0.5 will produce an indicated temperature change of +32 C. when an optical pyrometer is sighted upon a flat surface and a change of onl +1 C. when an optical pyrometer is sighted on the interior of a cavity with an L/R ratio of 13 to 1. Larger L/R ratios result in even smaller changes of indicated temperature with changes of surface emissivity.

The above comparison of temperature measurements has been described in connection with optical pyrometerssince there are fewer variable factors involved between the individual instruments than are present in connection with various individual radiation pyrometers, and for that reason uniform data on optical pyrometers is more readily obtainable. Due to the variable factors present in each radiation pyrometer instrument it is diflicult to provide a similar analysis for them; however, it may be stated that the variations occurring with a radiation pyrometer will be approximately four times as large as the variations produced with an optical pyrometer. Thus, in comparing the effects of the change of surface emissivity, a. change of emissivity from 0.4 to 0.5 will produce an indicated temperature change of approximately +128 C. when a radia-v tion pyrometer is sighted upon a flat surface and a change of approximately +4 C. when a radiation pyrometer is sighted upon the interior of acavity with an L/R ratio of 13 to 1.

From the above analysis it may readily be seen that by forming the liquid into an elongated cavity, in accordance with the present invention,

the effective emissivity of the liquid may bev greatly increased to closely approximate the emissivity of a black body and that any error in the pyrometer measurements of the true temperature of a liquid due to variations in the sur face emissivity thereof will be greatly reduced.

The term sighting as herein employed is not limited to observation by the human eye, but is used, as common in pyrometry, also to compre hend observation or sighting by any radiationresponsive element, such as a radiation pyrometer, photoelectric cell or equivalent device, pref-.

erably one which producedan electrical effect of magnitude representative of the temperature of the liquid under observation.

It shall be understood the invention is notlimited to the specific arrangements shown, and

that changes and modifications may be made within the scope of the appended claims.

What is claimed is:

1. Means for measuring the temperature of liquid comprising a body member having a flow passage for said liquid and having structure for imparting a rotary motion to the liquid in the passage to form axially thereof an elongated vortex closed at its bottom to provide black-body conditions therein, and a radiation-responsive measuring device for sighting axially of said passage for response to the black-body radiation from the vortex formed.

2. In combination with a radiation pyrometer for measuring the temperature of a liquid, a device for forming a vortex in a liquid, said device having a flow passage for said liquid with struc ture for imparting a rotary motion to the liquid in the passage to form axially thereof an elongated vortex closed at its bottom to provide black-body conditions within said vortex, and said radiation pyrometer being sighted axially of said vortex and its surrounding flow passage to convert said black-body radiation emanating 1 1 from said vortex into a direct indication of the true temperature of said liquid,

3 In combination with a radiation pyronieter for measuring th tem e u e o a iqu d stream a device for forming a vertex in said liquid stream comprising a body member having a flow passage therein, said flow passage having a channel portion and a circular cavity portion for receiving said liquid stream, said channel portion so dened t ct a d uid tream an ntially into said cavity portion for imparting a rotary motion to said liquid stream adequate to form a vortex therein, said cavity portion having a tubular discharge opening in its bottom for forming an elongated cavity in said vortex closed at the bottom and having an opening at the upper end thereof, said elongated cavity providing a black-body condition and serving as the target upon which said radiation pyrometer is s hted ax al y th eo t on t e b a k-body rad t n emanating f om said on ated av y into a d rect i dicat on r ondin with the tru temperature of said liquid stream.

Mean o ea u i e mper tur of a l qu d tr m und r blacky onditio s comp i g a y m mbe m unt d i a. s a n ry p i i n r r eiv ng t erein s id liquid stream fl w, d bo y m m er avin a channel an a u -s ed av t ormed the ein for passa e therethrough o id li u d. r m, aid. tunnelshaped cavity being provided with a tubular dis charge passage, said channel being designed to direct said liquid stream tangentially into said n h p d ca ty f r m rting a rotary motion to said liquid stream to form an elongated rt x h ing a c s d bo om, a d VQlteX having a suiiicient length to provide therein blackdy c nd t ons and a rad ationsp nsive e i g e ice positi ned n fix d relation with said body member and sighted along the x of nd in o sa d vor ex W thi which said black-body condit n xi t.-

n a gem nt for me su ing th u sur face temperature of a flowing liquid comprisin Structure including a b dy cavity and a dischar ifi e through whi h he quid flows and in wh c the liquid r ta m an .fo intro ucin a qu d into id dy cavity to ne side of said discharge orifice for imparting a rotary 119-. tion to the liquid as it flows through said structure to form a vortex in said liquid open to atmosphere at the top and effectively closed at the bottom to provide black-body conditions, said body cavity being of greater cross-sectional area than said discharge orifice, and a radiation-measuring device sighted into said vortex through said open-top thereof.

Mean or measuring the temp rature of a l qu d t eam de l ck-b dy condit ons com prising a vortex-forming devicefer providing an elongated cavity in a liquid stream comprising a body member, a funnel-shaped cavity termed in said body member and at least one inlet channel formed in said body member and being connected at one end to said cavity for passage through said channel to said cavity of said liquid stream, said channel being designed to direct said liquid stream tangentially into said funnelshaped cavity to impart a rotary motion to said liquid, said funnel-shaped cavity having a tubular discharge passage for forming said liquid into an elongated cavity, the cross-sectional area 01' said channel being large with respect to the cross-sectional area of said tubular discharge passage, and the length of said tubular discharge passage being about two to three times as great as the diameter of said tubular discharge passage to assure the elongated cavity to be formed in the liquid stream will be of suflicient length to be effectively closed at the bottom to provide therein black-body conditions.

'7. An arrangement according to claim 6 wherein there are provided a plurality of channels passing through the wall of said body member at spaced locations for directing the liquid stream tangentially into said funnel-shaped cavity to impart a rotary motion to said liquid.

8. An arrangement according to claim 6 wherein said channel is characterized by joining said funnel-shaped cavity at a point tangent to the circumference thereof and extending completely therearound forming a flat ledge of decreasing width, the outer edge thereof having the curvature of a spiral.

9 An arrangement according to claim 6 including an overflow passage flow-connected with said channel for controlling the maximum flow through said channel, and means bridging said channel positioned between said overflow passage and said funnel-shaped cavity :for slgimming slag from the surface of the liquid passing thereunder to said funnel-shaped cavity,

References Cited in the file of this patent UNIT D TAT S 

